Upload
others
View
1
Download
0
Embed Size (px)
Citation preview
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
1 / 43
EV12DS480AZP – Heavy Ions Test Report
Revision date : 06/Sep/2019
Author : BONNET OLIVIER
Scope : BUSINESS UNIT BMS
__________________________________
Last revision approved by :
Approved by Approbation Status Date
Mme. NIKITINE Carine M PILARD Romain
Yes Yes
09/09/2019 09/09/2019
___ _______________________________
Whilst Teledyne e2v Semiconductors SAS has taken care to ensure the accuracy of the information contained
herein it accepts no responsibility for the consequences of any use thereof and also reserves the right to
change the specification of goods without notice.
Teledyne e2v Semiconductors SAS accepts no liability beyond the set out in its standard conditions of sale in
respect of infringement of third party patents arising from the use of the devices in accordance with
information contained herein.
Teledyne e2v Semiconductors SAS, avenue de Rochepleine 38120 Saint-Egrève, France
Holding Company: Teledyne e2v Semiconductors SAS
Telephone: +33 (0)4 76 58 30 00
Contact Teledyne e2v by e-mail: [email protected] or visit www.teledyne-e2v.com for global
sales and operations centers.
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
2 / 43
1 DOCUMENT AMENDMENT RECORD
Author Issue Date Reason for change
BONNET Olivier A Creation
BONNET Olivier A.1 Curves added, text corrections
BONNET Olivier A.2 Copyright added
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
3 / 43
INDEX
1 DOCUMENT AMENDMENT RECORD ........................................................................................ 2
2 PURPOSE ................................................................................................................................... 4
3 GLOSSARY ................................................................................................................................ 4
4 APPLICABLE AND REFERENCE DOCUMENTS ....................................................................... 5
5 EXECUTIVE SUMMARY ............................................................................................................. 5
5.1 LOT DESCRIPTION ................................................................................................................... 5
5.2 HEAVY IONS ........................................................................................................................... 6
6 HEAVY IONS TEST .................................................................................................................... 7
6.1 IRRADIATION FACILITY ............................................................................................................. 7
6.2 COMPONENTS IMPLEMENTATION ............................................................................................. 9
6.3 IMPLEMENTATION EQUIPMENT ............................................................................................... 11
6.4 MEASUREMENT EQUIPMENT .................................................................................................. 11
6.5 SOFTWARE USED ................................................................................................................. 11
6.6 IMPLEMENTATION AND MEASUREMENT SYNOPTIC : TEST1 ....................................................... 13
6.7 IMPLEMENTATION AND MEASUREMENT SYNOPTIC : TEST2 ....................................................... 15
6.8 COMPONENTS CONFIGURATION ............................................................................................. 16
6.9 TEST SETUP ......................................................................................................................... 17
6.10 DOSIMETRY ......................................................................................................................... 19
7 RESULTS .................................................................................................................................. 20
7.1 SEL RESULTS ...................................................................................................................... 20
7.2 SET/SEFI RESULTS FOR TEST1 ........................................................................................... 21
7.3 SEFI RESULTS FOR TEST2 ................................................................................................... 30
7.4 SET DURATION .................................................................................................................... 34
8 SEE CONCLUSION .................................................................................................................. 40
9 APPENDIX ................................................................................................................................ 41
9.1 DETAILS OF EQUIPMENT USED FOR THE MEASUREMENTS ........................................................ 41
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
4 / 43
2 PURPOSE
The present document presents the SEE results of the TELEDYNE e2v EV12DS480AZP DAC device. The heavy ions test performed at the RADEF, the week 16 of 2019.
3 GLOSSARY
CREME Cosmic Ray Effects on Micro-Electronics DAC Digital-to-Analog Converter DC Direct Current DSP Digital Signal Processor DUT Device Under Test HF High Frequency HIF Heavy Ions Facility IUCM Input Under Clocking Mode LED Light-Emitting Diode LET Linear Energy Transfer MTBF Mean Time Between Failure MUX MUltipleXer NRTZ Narrow Return To Zero NRZ Non Return to Zero OCDS Output Clock Division Select Function OMERE Modelization tool for extern radiative environment PSS Phase Shift Select Function RADEF RADiation Effects Facility (Jyväskylä University laboratory, Finland) RF Radio Frequency RTZ Return To Zero SEE Single Event Effect SEFI Single Event Functional Interrupt SEL Single Event Latchup SET Single Event Transient In Graphs:
- Minimum: Minimum value of each parts (except reference parts) - Maximum: Maximum value of each parts (except reference parts) - Mean: Mean value of each parts (except reference parts) - Median: Median value of each parts (except reference parts), half of the devices are
upper this limit, half are under
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
5 / 43
4 APPLICABLE AND REFERENCE DOCUMENTS
The documents applicable to this work are the following:
Document No. Rev Title
MIL-STD-883 J Test Method Standard Microcircuits ASTM-F 1192 2011 Standard Guide for the Measurement of Single Event Phenomena
(SEP) Induced by Heavy Ion Irradiation of Semiconductor Devices
EIA/ JESD57 Dec. 1996
Test Procedure for the Management of Single-Event Effects in Semiconductor Devices from Heavy Ion Irradiation
DS 60S 217580 A.1 Datasheet EV12DS480AZP Low power 12-bit 8GSps Digital to Analog Converter with 4/2:1 Multiplexer
5 EXECUTIVE SUMMARY
5.1 Lot description
Reference EV12DS480AZP
Package FpBGA196
Function Low power 12bit 8Gsps DAC
Technology Infineon B7HF200
Diffusion Lot No. RU516515
Mfr. No. EV12DS480AMZP-N1
Mask Lot VN62
Front End Date Code 1527
Manufacturer Teledyne E2V
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
6 / 43
5.2 Heavy ions
Teledyne e2v has performed Heavy ions tests on the EV12DS480AZP DAC device to evaluate the sensitivity to the Single Event Latch up (SEL) & Single Event Effects (SEU, SEFI, SET) for various clock, 4.5GHz, 6GHz and 8GHz. A special code has been developed to manage automatically the SEFI by re-programming the registers.
Tests were performed at the RADEF, Jyväskylä, Finland, on the 15th, 16th and on the 17th of April 2019.
o No SEL was detected during the irradiation with a LET of 60 MeV.cm²/mg, with no tilt.
3 DUT were tested at Tj=135°C, with maximum power supplies + 10%.
o SET were observed during the irradiation from 3.6 MeV.cm²/mg to 69.3 MeV.cm²/mg, at room temperature and typical power supplies.
o SEFI were observed during the irradiation from 3.6 MeV.cm²/mg to 69.3 MeV.cm²/mg but all these SEFI were successfully managed by software
o There is no significant gap between SET/SEFI cross sections obtained in the different modes.
o There is no significant gap between SET/SEFI cross sections obtained for DACOUT and DSPCLK.
o There is no impact of the clock frequency on the device, the SEFI cross section remains the same whatever is the clock, 4.5GHz, 6GHz or 8GHz
These SEE results show that the EV12DS480 DAC, can be used as a space product.
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
7 / 43
6 HEAVY IONS TEST
6.1 Irradiation facility
An irradiation tests was performed at Jyväskylä (Finland) on the 15th, 16th and on the 17th of April 2019 a maximum LET of 60 MeV.cm²/mg without tilt, and 69.3 MeV.cm²/mg with tilt (30°).
Config Cocktail
A MeV Ion Symbol Tilt
Energy
(MeV)
Range
(µm(Si))
LET
(MeV/mg/cm²)
at Surface
LET
(MeV/mg/cm²)
Bragg peak
1 9.3 Neon Ne 0° 186 146 3.63 5.9 (@198)
2 9.3 Iron Fe 0° 523 97 18.5 29.3 (@77)
3 9.3 Krypton Kr 0° 768 94 32.2 41 (@69)
4 9.3 Xenon Xe 0° 1217 89 60.0 69.2 (@48)
5 9.3 Xenon Xe 18° 1217 89 63.1
6 9.3 Xenon Xe 30° 1217 89 69.3
7 16.3 Oxygen 17
O6+
0° 284 481 1.52 7.17 (@477)
8 16.3 Iron 57
Fe20+
0° 941 214 13.3 29.3 (@192)
9 16.3 Xenon 126
Xe44+ 0° 2059 157 48.5 69.3 (@119)
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
8 / 43
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
9 / 43
6.2 Components implementation
The devices have been decaped by using a chemical process.
The opened devices have been soldered on Teledyne E2v evaluation boards which have been used to perform the heavy ions tests. These evaluation boards include a FPGA used to generate the pattern to the DAC (DUT). DACOUT and DSPCLK have been tested during the Heavy Ions Test.
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
10 / 43
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
11 / 43
6.3 Implementation equipment
The implementation equipment is described in the table below.
6.4 Measurement equipment
Designation Reference Identification Valididty date Scope Teledyne Lecroy WR640Zi ON067 08/04/2021 Scope Teledyne Lecroy WR620Zi ON063 31/08/2020
Multimeter Agilent U1772A Mu086 Checked before use Power Supply Fluke PM2811 QM3549 Checked before use
Syntheyser Signal generator QM4217 20/02/2020
6.5 Software used
Designation Comments
Setup_CaracDAC12_1_3_0
E2V provider
Carac DAC 12 bit
FW : 1.1.0
FPGA : 2.0
Used for control DAC (Via USB interface)
GenICam 1.1
E2V provider
V1.1
Used in order to install necessary drivers.
THIMS - SEFI
E2V provider
Used to check SEFI signal from scope (Via USB interface) and to
program DAC register (via USB interface) in case of SEFI detection.
This soft has been developed with the experience of the SEFI
management acquired during the first Heavy Ions run.
TightVnc
Remote controller
V2.8.5
Used to perform a remote control of the scope. (Via Ethernet
interface)
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
12 / 43
Figure 1: Setup_CaracDAC12_1_3_0
Figure 2: THIMS - SEFI
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
13 / 43
6.6 Implementation and measurement synoptic : Test1
Principle of SEE detection Detecting SEE on microwave periodical signals implies to remove the periodical component of the output signal, and emphasize the transient component. The resulting signal allows triggering an oscilloscope each time a SEE occurs. In order to remove the periodical part of a signal coming out of a component under test, a mixer is used. This type of circuit allows frequency transposition, which transposes a signal whose frequency is centered on an initial frequency to another frequency without altering its bandwidth.
The output signal is then filtered in order to keep either its higher frequency or its lower frequency band. In the present case, the output signal of the DUT is mixed with a signal of same spectral content, in order to get a low pass filtered signal of 0 Hz that is a DC signal. Therefore this signal is composed of all energy other than that of the input signal. In other words it only consists of the transient part, non-sinusoidal part of the signal, coming from the disturbance impacting the DUT during heavy ion experiments. Setup diagram The simplified diagram presented below shows the SEL and SET/SEFI setup of the experimentation.
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
14 / 43
Figure 3: SEL Test
Figure 4: SET/SEFI Test
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
15 / 43
6.7 Implementation and measurement synoptic : Test2
For this test, both output (DACOUT & DSPCLK) were checked with a scope. The scope was located in the bunker but was controlled from the control room. DACOUT output was checked by a scope, with a min-max detection for the static pattern and with an envelope detection for the dynamic pattern. Unfortunately, the scope has saved several time the SET so, for this test, only the SEFI are evaluated in this report.
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
16 / 43
6.8 Components configuration
Component configuration depends on several parameters, which are listed in the following paragraphs. Input clock frequency • Values: 4.5 GHz for Test1, 4.5, 6 and 8GHz for Test2; • The input clock frequency is generated by a signal generator. It feeds the EV12DS4x0ZPY evaluation board. Input signal : Test1 • Dynamic pattern: sine wave at 100 MHz frequency; Input signal : Test2 Two patterns were used for this test:
- Static: Middle code pattern - Dynamic : Sin pattern
Junction temperature
Junction Temperature
SEL SEE/SEFI
135°C 125°C
Power supply
Power supply
SEL SEE/SEFI
VCCA5 = 5V + 10% VCCA5 = 5V
VCCD = 3.3V + 10% VCCD = 3.3V
VCCA3 = 3.3V + 10% VCCA3 = 3.3V
Output mode 4 modes have been used
The mode was set by using the Teledyne e2v software
mode Mux OCDS IUCM Pss RPW RPB GA
NRZ 4 0 00 111 0 0 200
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
17 / 43
NRTZ 4 0 00 111 1 1 200
RTZ 4 0 00 111 1 1 200
RF 4 0 00 111 1 1 200
6.9 Test setup
Before each irradiation run, the proper operation of the DUT was checked. For each run, any detected event causes the recording of all signals listed in the table below.
Signals
Channel 1 Channel 2 Channel 3 Channel 4 Aux
DSPclk SEFI trigger DACout SET trigger Not used
SEL Latchup has been monitored on the following DUT power supplies: • VCCA5 • VCCD • VCCA3 Tests have been done at the maximum operating temperature + 10C (135 °C).
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
18 / 43
Latchup detection and cut-off board were set to detect an increase of 20% of the nominal current consumption value. Each time a latchup would occur, the system would switch off the power supply in less than 150 µs after the detection. SET SET detection has been performed thanks to a detection board. The detection board has an attenuation of 14 dB on single-ended channels, and 10 dB on differential channels. Each detection level is set according to the observed trigger signal in order to be as close as possible to the trigger level. The conversion of differential signals to single-ended signal is made with baluns, located on the detection board. The minimum sensitivity of this system was defined experimentally:
Sensitivity of the SET detection system Time min. Amplitude min.
DACOUT ≈ 3 ns 40 mV
DSPCLK ≈ 5 ns 100 mV
SEFI SEFI detection is provided by specific signals (one for DACOUT and one for DSPCLK). If necessary a buzzer could be positioned on the control desk. The buzzer rings when a SEFI occurs. This detection remained active during all the campaign. SEFI detection (Alert/ signal) is checked by E2V THIMS software. SEFI have been classified in term of impact on the device.
SEFI 1 Solved by re-programming the
registers
SEFI 2 Solved by using the RESET
SEFI 3 Solved by switching-off the device
TEST LEVEL For SEL research, the test is stopped when a fluency of 107 ions.cm-2 is reached, or when at least 100 events are detected.
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
19 / 43
For SET research, the test is stopped when a fluency of 106 ions.cm-2 is reached, or when at least 100 events are detected.
6.10 Dosimetry
Dosimetry was provided by the RADEF. Fluency, irradiation times and deposited ionizing
dose were provided for each run and presented in the following tables.
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
20 / 43
7 RESULTS
During this campaign, we managed the SEFI with an automatic soft which was programming
the registers. Only SEFI 1 were detected during this campaign.
7.1 SEL Results
The SEL test was performed at 135°C and at maximum supply voltage + 10% with 3 devices.
No Latch-Up were observed during this test under Xenon irradiation with a total fluence
equal to 107particles.cm-2, with a particle angle of 0° (LET = 60 MeV.cm²/mg) and 18° (LET =
63 MeV.cm²/mg).
Docum
ent
refe
rence
Is
sue
NE
13S
218133
A.2
C
op
yri
gh
t T
ele
dyn
e e
2v 2
01
9
21 / 4
3
7.2
S
ET
/SE
FI
Resu
lts f
or
Test1
Docum
ent
refe
rence
Is
sue
NE
13S
218133
A.2
C
op
yri
gh
t T
ele
dyn
e e
2v 2
01
9
22 / 4
3
Docum
ent
refe
rence
Is
sue
NE
13S
218133
A.2
C
op
yri
gh
t T
ele
dyn
e e
2v 2
01
9
23 / 4
3
Docum
ent
refe
rence
Is
sue
NE
13S
218133
A.2
C
op
yri
gh
t T
ele
dyn
e e
2v 2
01
9
24 / 4
3
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
25 / 43
Figure 5 : SET Cross-section Vs LET for DACOUT, DUT1, Dynamic pattern
Figure 6 : SET Cross-section Vs LET for DACOUT, DUT2, Dynamic pattern
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
26 / 43
Figure 7 : SET Cross-section Vs LET for DSPCLK, DUT1, Dynamic pattern
Figure 8 : SET Cross-section Vs LET for DSPCLK, DUT2, Dynamic pattern
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
27 / 43
Figure 9 : SET Cross-section vs. LET for DACOUT/DSPCLK signals DUT 1: dynamic pattern in NRZ, NRTZ, RTZ and RF modes.
Figure 10 : SEFI Cross-section vs. LET for DACOUT/DSPCLK signals DUT1: dynamic pattern in NRZ, NRTZ, RTZ and RF modes
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
28 / 43
Figure 11 : SEE Cross-section vs. LET for DACOUT/DSPCLK signals DUT1: dynamic pattern in NRZ,
NRTZ, RTZ and RF modes
Figure 12 : SET Cross-section vs. LET for DACOUT/DSPCLK signals DUT2: dynamic pattern in NRZ,
NRTZ, RTZ and RF modes
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
29 / 43
Figure 13 : SEFI Cross-section vs. LET for DACOUT/DSPCLK signals DUT2: dynamic pattern in NRZ,
NRTZ, RTZ and RF modes
Figure 14 : SEE Cross-section vs. LET for DACOUT/DSPCLK signals DUT2: dynamic pattern in NRZ, NRTZ, RTZ and RF modes
All the SEFI are SEFI 1, which means that they have been solved using the software, by
writing into the registers (no reset, no reboot, no power down/up).
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
30 / 43
7.3 SEFI Results for Test2
Run Number DUT Flux Fluence Ion LET Dose Fclock Pattern IUCM Mode SEFI Commentaire
1-->7 4 4,72E+06 Xe 60 4,25E+00 4,5 Mil 1 NRTZ Setup with the static pattern
8 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 4,5 Mil 1 NRZ 29
9 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 4,5 Mil 1 NRTZ 38
10 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 4,5 Mil 1 RTZ 34
11 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 4,5 Mil 1 RF 14
12 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 6 Mil 1 NRZ 20
13 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 6 Mil 1 NRTZ 19
14 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 6 Mil 1 RTZ 20
15 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 6 Mil 1 RF 25
16 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 8 Mil 2 NRZ 34
17 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 8 Mil 2 NRTZ 24
18 4 2,00E+03 4,20E+05 Xe 60 3,78E-01 8 Mil 2 NRZ Wrong Mode
19 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 8 Mil 2 RTZ 34
20 4 2,00E+03 1,00E+06 60 9,00E-01 8 Mil 2 RF 30
21-->22 4 2,00E+03 2,11E+05 Xe 60 1,90E-01 Setup with the Sin pattern
23 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 4,5 Sin 1 NRZ 43
24 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 6 Sin 1 55
25 4 2,00E+03 1,00E+06 Xe 60 9,00E-01 8 Sin 2 51 All the SEFI are SEFI 1, which means that they have been solved using the software, by writing into the registers (no reset, no reboot, no power down/up).
Figure 15: SEFI Cross Section Vs Clock Frequency with a LET = 60 Mev/mg/cm
2
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
31 / 43
Total ionizing dose received by each component in the campaign:
DUT 1 (Board SN01) : 68 Krad(Si).
DUT 2 (Board SN02) : 59.8 Krad(Si).
DUT 3 (Board SN04) : 48.6 Krad(Si).
DUT 4 (Borad SN03) : 18.3 Krad(Si)
The Weibull fit equation is given by the following formula:
The table below summarizes the worst case Weibull fit parameters for DACOUT and DSPCLK, for
both dynamic and static pattern. Both SEE rate and MTBF calculations were performed with OMERE
software from parameters detailed in the table hereafter.
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
32 / 43
Test Conditions Weibull Fit Parameters SEE Rate Calculation
FClock
(GHz) Output Pattern
W
(MeV.cm2/mg)
S LET threshold L0
(MeV.cm2/mg)
Cross-
Section
Sat (cm2)
Mission (GEO) Rate/Day MTBF
(Days)
4.5 DACOUT
(SET) Dynamic 40 1.6 1.50E-2 3.25E-5
M3
15 years 1.58E-4 6329
M8
16 Days 6.26e-2 16
4.5 DSPCLK (SET) Dynamic 40 1.6 1.50E-2 2E-5
M3
15 years 9.62e-5 10395
M8
16 Days 3.45e-2 30
4.5 DACOUT
(SEE) Dynamic 40 1.6 1.50E-2 5.68E-5
M3
15 years 2.80e-4 3571
M8
16 Days 1.23e-1 8.1
4.5 DSPCLK (SEE) Dynamic 40 1.6 1.50E-2 2.21E-5
M3
15 years 1.07e-4 9346
M8
16 Days 3.92e-2 25.51
4.5 DACOUT
(SEFI) Dynamic 40 1.6 1.50E-2 2.44E-5
M3
15 years 1.18e-4 8474
M8
16 Days 4.41e-2 22.7
4.5 DSPCLK
(SEFI) Dynamic 40 1.6 1.50E-2 1.35E-5
M3
15 years 6.43e-5 15552
M8
16 Days 2.11e-2 47.4
Figure 16: Heavy ion SEE Rate Calculation with OMERE
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
33 / 43
Orbit GEO (35870 km)
Radiative Environment CREME 86 – M3 – Cosmic Rays Solar Min CREME 86 – M8 – Solar Eruption
– Worst-Case Flux
Mission Duration 15 years 16 days
Magnetospheric Cut-Off Without
Shielding 1 g.cm-2
Number of Cells 12
Cell Depth 6 µm
Figure 17: Calculation parameters with OMERE
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
34 / 43
7.4 SET Duration
The following graphs plot the events depending on their amplitude and duration.
Figure 18 : Maximum amplitude Vs maximum duration for DSPCLK events @ 4.5GHz
Figure 19 : Maximum amplitude Vs maximum duration for DACOUT events @ 4.5GHz
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
35 / 43
Some examples of events are presented on the following pages. The attenuation on DACOUT induced by the detection system is 10 dB, the attenuation on DSPCLK is 11 dB. These examples show a lot of possible waveforms in case of SET induced certainly by DAC registers failures.
Figure 20 : DSPCLK SET example Run 10 (NRZ mode, LET 60 MeV/mg/cm2)
Figure 21 : DSPCLK SET example Run 18 (NRTZ mode, LET 63.5 MeV/mg/cm2, tilt 18°)
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
36 / 43
Figure 22 : DSPCLK SET example Run 20 (Mode RF, LET 32.1 MeV/mg/cm2)
Figure 23 : DSPCLK SET example Run 22 (Mode NRTZ, LET 18.5 MeV/mg/cm2)
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
37 / 43
Figure 24 : DSPCLK SET example Run 23 (Mode NRZ, LET 3.6 MeV/mg/cm2)
Figure 25 : DACOUT SET example Run 10 (NRZ mode, LET 60 MeV/mg/cm2)
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
38 / 43
Figure 26 : DACOUT SET example Run 18 (NRTZ, LET 63.5 MeV/mg/cm2, tilt 18°)
Figure 27 : DACOUT SET example Run 20 (Mode RF, LET 32.1 MeV/mg/cm2)
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
39 / 43
Figure 28 : DACOUT SET example Run 22 (LET 18.5 MeV/mg/cm2)
Figure 29 : DACOUT SET example Run 23 (Mode NRZ, LET 3.6 MeV/mg/cm2)
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
40 / 43
8 SEE CONCLUSION
Teledyne e2v has performed a Heavy ions tests on the EV12DS480AZP DAC device to evaluate the sensitivity to the Single Event Latch up (SEL) & Single Event Effects (SEU, SEFI, SET) for various clock, 4.5GHz, 6GHz and 8GHz. A special code has been developed to manage automatically the SEFI by re-programming the registers.
Tests were performed at the RADEF, Jyväskylä, Finland, on the 15th, 16th and on the 17th of April 2019.
o No SEL was detected during the irradiation with a LET of 60 MeV.cm²/mg, with no tilt.
3 DUT were tested at Tj=135°C, with maximum power supplies + 10%.
o SET were observed during the irradiation from 3.6 MeV.cm²/mg to 69.3 MeV.cm²/mg, at room temperature and typical power supplies.
o SEFI were observed during the irradiation from 3.6 MeV.cm²/mg to 69.3 MeV.cm²/mg but all these SEFI were successfully managed by software
o There is no significant gap between SET/SEFI cross sections obtained in the different modes.
o There is no significant gap between SET/SEFI cross sections obtained for DACOUT and DSPCLK.
o There is no impact of the clock frequency on the device, the SEFI cross section remains the same whatever is the clock, 4.5GHz, 6GHz or 8GHz
These SEE results show that the EV12DS480 DAC, can be used as a space product.
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
41 / 43
9 APPENDIX
9.1 Details of equipment used for the measurements
Figure 30 : Test Instrumentation (1)
Figure 31 : Test Instrumentation (2)
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
42 / 43
Figure 32 : Die Marking DUT1
Figure 33 : Die Marking DUT2
Document reference Issue
NE 13S 218133
A.2
Copyright Teledyne e2v 2019
43 / 43
Figure 34 : 135°C mini-MARTA view